Reaction Motors Division of Thiokol's XLR99-RM-1 was the throttleable, single-chamber rocket engine developed specifically for the piloted X-15. NASA records anhydrous ammonia and liquid oxygen propellants, 19,200–57,200 lbf at 40,000 feet, 256–276 s specific impulse, and first XLR99-powered flight in November 1960; the engine is recorded as a retired historical model with no additional installation inferred.